Książki na temat „AERODYNAMICS EFFECT”

1913-, Young A. D., i North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., red. Scale effects on aircraft and weapon aerodynamics. Neuilly sur Seine, France: AGARD, 1994.

Haines, A. B. Scale effects on aircraft and weapon aerodynamics. Neuilly sur Seine: Agard, 1994.

McMillin, S. Naomi. Effect of planform and body on supersonic aerodynamics of multibody configurations. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

McMillin, S. Naomi. Effect of planform and body on supersonic aerodynamics of multibody configurations. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Rozhdestvensky, Kirill V. Aerodynamics of a Lifting System in Extreme Ground Effect. Berlin, Heidelberg: Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-04240-3.

T, Suit William, i Langley Research Center, red. Effect of transition aerodynamics on aeroassist flight experiment trajectories. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Raman, G. Initial turbulence effect on jet evolution with and without tonal excitation. [Washington, DC]: National Aeronautics and Space Administration, 1987.

Darden, Christine M. Effect of leading-edge load constraints on the design and performance of supersonic wings. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Darden, Christine M. Effect of leading-edge load constraints on the design and performance of supersonic wings. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Althoff, Susan L. Effect of blade planform variation on a small-scale hovering rotor. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Center, Ames Research, red. Effect of non-equilibrium flow chemistry on the heating distribution over the MESUR forebody during a Martian entry. [Moffett Field, Calif.]: NASA Ames Research Center, 1992.

Center, Ames Research, red. Effect of non-equilibrium flow chemistry on the heating distribution over the MESUR forebody during a Martian entry. [Moffett Field, Calif.]: NASA Ames Research Center, 1992.

Center, Ames Research, red. Effect of non-equilibrium flow chemistry on the heating distribution over the MESUR forebody during a Martian entry. [Moffett Field, Calif.]: NASA Ames Research Center, 1992.

Curry, Robert E. Dynamic ground effect for a cranked arrow wing airplane. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

C, Pontonides H., i United States. National Aeronautics and Space Administration., red. Effect of variable-inlet guide vanes on the operating characteristics of a tilt nacelle-inlet powered fan model. [Washington, DC: National Aeronautics and Space Administration, 1987.

C, Pontonides H., i United States. National Aeronautics and Space Administration., red. Effect of variable-inlet guide vanes on the operating characteristics of a tilt nacelle-inlet powered fan model. [Washington, DC: National Aeronautics and Space Administration, 1987.

L, Kelley Henry, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, red. Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Sanford, Fleeter, i Lewis Research Center, red. The predicted effect of aerodynamic detuning of coupled bending-torsion unstalled supersonic flutter. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Henderson, William P. Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds. Hampton, Va: Langley Research Center, 1987.

R, Burley James, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

R, Dudley Michael, Schell Charles J i Ames Research Center, red. Hover in-ground-effect testing of a full-scale, tilt-nacelle V/STOL model. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

K. B. M. Q. Zaman. Effect of 'delta tabs' on mixing and axis switching in jets from asymmetric nozzles. [Washington, DC: National Aeronautics and Space Administration, 1994.

R, Dudley Michael, Schell Charles J i Ames Research Center, red. Hover in-ground-effect testing of a full-scale, tilt-nacelle V/STOL model. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

R, Dudley Michael, Schell Charles J i Ames Research Center, red. Hover in-ground-effect testing of a full-scale, tilt-nacelle V/STOL model. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

Curry, Robert E. An in-flight investigation of ground effect on a forward-swept wing airplane. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

J, Moulton Bryan, Kresse John i Dryden Flight Research Facility, red. An in-flight investigation of ground effect on a forward-swept wing airplane. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

Curry, Robert E. An in-flight investigation of ground effect on a forward-swept wing airplane. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

Curry, Robert E. An in-flight investigation of ground effect on a forward-swept wing airplane. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

Canada, Canada Public Works. Investigations into the effect of high winds on vehicular traffic. Otawa: Public Works Canada, 1988.

T, Carson George, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

T, Carson George, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Effect of afterbody geometry on aerodynamic characteristics of isolated nonaxisymmetric afterbodies at transonic Mach numbers. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

1933-, Nayfeh Ali Hasan, Ragab Saad i United States. National Aeronautics and Space Administration., red. Effect of wall cooling on the stability of compressible subsonic flows over smooth humps and backward-facing steps. Blacksburg, Va: Dept. of Engineering Science and Mechanics, Virginia Polytechnic Institute and State University, 1989.

Ramesh, Pankajakshan, i United States. National Aeronautics and Space Administration., red. Propulsion/airframe interference for ducted propfan engines with ground effect. [Washington, DC: National Aeronautics and Space Administration, 1994.

Farokhi, Saeed. Effect of initial tangential velocity distribution on the mean evolution of a swirling turbulent free jet. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Center, Ames Research, red. A two dimensional study of rotor/airfoil interaction in hover. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Center, Langley Research, red. Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Nissim, E. Effect of control surface mass unbalance on the stability of a closed-loop active control system. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

R, Booth Earl, Takallu Mohammad Ali 1948- i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Effect of pylon wake with and without pylon blowing on propeller thrust. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

G, Murri Daniel, Lanser Wendy R i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

G, Murri Daniel, Lanser Wendy R i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Jacob, Klaus. Advanced method for computing the flow around wings with rear separation and ground effect. Gottingen: DFVLR Institut fur Theoretische Stromungsmechanik, 1986.

Binek, Alexander P. A study of the aerodynamic effect of an obstacle attached to the leeward side of a sphere in low-speed flow. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2002.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

A, Campbell Bryan, Monta William J i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Bezos, Gaudy M. Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift. Hampton, Va: Langley Research Center, 1993.

A, Campbell Bryan, Monta William J i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, red. Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

A, Campbell Bryan, Monta William J i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Development of a large-scale, outdoor, ground-based test capability for evaluating the effect of rain on airfoil lift. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Penland, Jim A. Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Mineck, Raymond E. Application of two procedures for dual-point design of transonic airfoils. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Mineck, Raymond E. Application of two procedures for dual-point design of transonic airfoils. Hampton: National Aeronautics and Space Administration, Langley Research Center, 1994.